Moving expansion waves: Difference between revisions

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\subsection{Moving Expansion Waves}
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==== Moving Expansion Waves ====


\noindent The expansion wave propagation into the driver section in a shock tube can be described using characteristic lines.\\
The expansion wave propagation into the driver section in a shock tube can be described using characteristic lines.


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\noindent The expansion is propagating into stagnant fluid in region four (the driver section), which means that the flow properties ahead of the expansion wave are constant. \\
The expansion is propagating into stagnant fluid in region four (the driver section), which means that the flow properties ahead of the expansion wave are constant.


\begin{equation*}
{{NumEqn|<math>
J^+_a=J^+_b
J^+_a=J^+_b
\end{equation*}\\
</math>}}


\noindent $J^+$ invariants constant along $C^+$ characteristics\\
<math>J^+</math> invariants constant along <math>C^+</math> characteristics


\begin{equation*}
{{NumEqn|<math>
J^+_a=J^+_c=J^+_e
J^+_a=J^+_c=J^+_e
\end{equation*}\\
</math>}}


\begin{equation*}
{{NumEqn|<math>
J^+_b=J^+_d=J^+_f
J^+_b=J^+_d=J^+_f
\end{equation*}\\
</math>}}


\noindent Since $J^+_a=J^+_b$ this also implies $J^+_e=J^+_f$. In fact, since the flow properties ahead of the expansion are constant, all $C^+$ lines will have the same $J^+$ value.\\
Since <math>J^+_a=J^+_b</math> this also implies <math>J^+_e=J^+_f</math>. In fact, since the flow properties ahead of the expansion are constant, all <math>C^+</math> lines will have the same <math>J^+</math> value.


\noindent $J^-$ invariants constant along $C^-$ characteristics\\
<math>J^-</math> invariants constant along <math>C^-</math> characteristics


\begin{equation*}
{{NumEqn|<math>
J^-_c=J^-_d
J^-_c=J^-_d
\end{equation*}\\
</math>}}


\begin{equation*}
{{NumEqn|<math>
J^-_e=J^-_f
J^-_e=J^-_f
\end{equation*}\\
</math>}}


\begin{equation*}
{{NumEqn|<math>
\left.
\left.
\begin{aligned}
\begin{aligned}
Line 54: Line 67:
\end{aligned}
\end{aligned}
\right\}\Rightarrow u_e=u_f \Rightarrow a_e=a_f
\right\}\Rightarrow u_e=u_f \Rightarrow a_e=a_f
\end{equation*}\\
</math>}}


\noindent Due to the fact the $J^+$ is constant in the entire expansion region, $u$ and $a$ will be constant along each $C^-$ line.\\
Due to the fact the <math>J^+</math> is constant in the entire expansion region, <math>u</math> and <math>a</math> will be constant along each <math>C^-</math> line.


\noindent The constant $J^+$ value can be used to obtain relations for the variation of flow properties through the expansion region. Evaluation of the $J^+$ invariant at any position within the expansion region should give the same value as in region 4.\\
The constant <math>J^+</math> value can be used to obtain relations for the variation of flow properties through the expansion region. Evaluation of the <math>J^+</math> invariant at any position within the expansion region should give the same value as in region 4.


\begin{equation*}
{{NumEqn|<math>
u+\frac{2a}{\gamma-1}=u_4+\frac{2a_4}{\gamma-1}=0+\frac{2a_4}{\gamma-1}
u+\frac{2a}{\gamma-1}=u_4+\frac{2a_4}{\gamma-1}=0+\frac{2a_4}{\gamma-1}
\end{equation*}\\
</math>}}


\noindent and thus\\
and thus


\begin{equation}
{{NumEqn|<math>
\frac{a}{a_4}=1-\frac{\gamma-1}{2}\left(\frac{u}{a_4}\right)
\frac{a}{a_4}=1-\frac{\gamma-1}{2}\left(\frac{u}{a_4}\right)
\label{eq:expansion:a}
</math>}}
\end{equation}\\


\noindent Eqn. \ref{eq:expansion:a} and $a=\sqrt{\gamma RT}$ gives\\
Eqn. \ref{eq:expansion:a} and <math>a=\sqrt{\gamma RT}</math> gives


\begin{equation}
{{NumEqn|<math>
\frac{T}{T_4}=\left[1-\frac{\gamma-1}{2}\left(\frac{u}{a_4}\right)\right]^2
\frac{T}{T_4}=\left[1-\frac{\gamma-1}{2}\left(\frac{u}{a_4}\right)\right]^2
\label{eq:expansion:b}
</math>}}
\end{equation}\\


\noindent Using isentropic relations, we can get pressure ratio and density ratio\\
Using isentropic relations, we can get pressure ratio and density ratio


\begin{equation}
{{NumEqn|<math>
\frac{p}{p_4}=\left[1-\frac{\gamma-1}{2}\left(\frac{u}{a_4}\right)\right]^{2\gamma/(\gamma-1)}
\frac{p}{p_4}=\left[1-\frac{\gamma-1}{2}\left(\frac{u}{a_4}\right)\right]^{2\gamma/(\gamma-1)}
\label{eq:expansion:b}
</math>}}
\end{equation}\\


\begin{equation}
{{NumEqn|<math>
\frac{\rho}{\rho_4}=\left[1-\frac{\gamma-1}{2}\left(\frac{u}{a_4}\right)\right]^{2/(\gamma-1)}
\frac{\rho}{\rho_4}=\left[1-\frac{\gamma-1}{2}\left(\frac{u}{a_4}\right)\right]^{2/(\gamma-1)}
\label{eq:expansion:b}
</math>}}
\end{equation}\\

Latest revision as of 13:36, 1 April 2026

Moving Expansion Waves

The expansion wave propagation into the driver section in a shock tube can be described using characteristic lines.


The expansion is propagating into stagnant fluid in region four (the driver section), which means that the flow properties ahead of the expansion wave are constant.

Ja+=Jb+(Eq. 6.135)

J+ invariants constant along C+ characteristics

Ja+=Jc+=Je+(Eq. 6.136)
Jb+=Jd+=Jf+(Eq. 6.137)

Since Ja+=Jb+ this also implies Je+=Jf+. In fact, since the flow properties ahead of the expansion are constant, all C+ lines will have the same J+ value.

J invariants constant along C characteristics

Jc=Jd(Eq. 6.138)
Je=Jf(Eq. 6.139)
ue=12(Je++Je)uf=12(Jf++Jf)Je=JfJe+=Jf+}ue=ufae=af(Eq. 6.140)

Due to the fact the J+ is constant in the entire expansion region, u and a will be constant along each C line.

The constant J+ value can be used to obtain relations for the variation of flow properties through the expansion region. Evaluation of the J+ invariant at any position within the expansion region should give the same value as in region 4.

u+2aγ1=u4+2a4γ1=0+2a4γ1(Eq. 6.141)

and thus

aa4=1γ12(ua4)(Eq. 6.142)

Eqn. \ref{eq:expansion:a} and a=γRT gives

TT4=[1γ12(ua4)]2(Eq. 6.143)

Using isentropic relations, we can get pressure ratio and density ratio

pp4=[1γ12(ua4)]2γ/(γ1)(Eq. 6.144)
ρρ4=[1γ12(ua4)]2/(γ1)(Eq. 6.145)